00990nam0-2200313---450-99000876635040332120090331115707.088-203-1457-6000876635FED01000876635(Aleph)000876635FED0100087663520081126d1986----km-y0itay50------baitaITy-------001yyMotori endotermicimotori ad accensione per scintilla a carburazione e ad iniezione, motori ad accensione per compressione, Diesel lenti e veloci, motori rotativi, turbine a gas, teoria, costruzione, proveDante Giacosa14. ed. aggiornataMilanoU. Hoepli1986XXI, 848 p.ill.25 cm621.4319itaGiacosa,Dante901ITUNINARICAUNIMARCBK990008766350403321I29DINPADINPAMotori endotermici77986UNINA01936oam 2200517 a 450 991070037110332120110613103635.0(CKB)5470000002409274(OCoLC)730242320(EXLCZ)99547000000240927420110613d2010 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierA simplified model for detonation based pressure-gain combustors[electronic resource] /Daniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (13 pages) illustrations, colorNASA/TM ;2010-216821Title from title screen (viewed on June 13, 2011)."November 2010.""AIAA-2010-6717."Includes bibliographical references (pages 12-13).DetonationnasatGas turbinesnasatPulsed jet enginesnasatCombustion chambersnasatFlow distributionnasatReliability analysisnasatDetonation.Gas turbines.Pulsed jet engines.Combustion chambers.Flow distribution.Reliability analysis.Paxson Daniel E1386438NASA Glenn Research Center.AIAA/ASME/SAE/ASEE Joint Propulsion Conference(46th :2010 :Nashville, Tenn.)GPOGPOGPOBOOK9910700371103321A simplified model for detonation based pressure-gain combustors3498662UNINA